Remove trailing white space

.gitattributes

@@ -11,4 +11,4 @@
 
 # Denote all files that are truly binary and should not be modified.
 *.png binary
-*.jpg binary
+*.jpg binary

OpenHydraulics/Basic/BaseClasses/LossFactorData.mo

@@ -19,7 +19,7 @@ record LossFactorData
 This record defines the pressure loss factors of a pipe
 segment (orifice, bending etc.) with a minimum amount of data.
 If available, data should be provided for <b>both flow directions</b>,
-i.e., flow from port_a to port_b and from port_b to port_a, 
+i.e., flow from port_a to port_b and from port_b to port_a,
 as well as for the <b>laminar</b> and the <b>turbulent</b> region.
 It is also an option to provide the loss factor <b>only</b> for the
 <b>turbulent</b> region for a flow from port_a to port_b.
@@ -59,29 +59,29 @@ where
      &zeta; is constant and is given by \"zeta1\" and
      \"zeta2\" depending on the flow direction.<br>
      When the Reynolds number Re is below \"Re_turbulent\", the
-     flow is laminar for small flow velocities. For higher 
-     velocities there is a transition region from 
+     flow is laminar for small flow velocities. For higher
+     velocities there is a transition region from
      laminar to turbulent flow. The loss factor for
      laminar flow at small velocities is defined by the often occuring
      approximation c0/Re. If c0 is different for the two
-     flow directions, the mean value has to be used 
+     flow directions, the mean value has to be used
      (c0 = (c0_ab + c0_ba)/2).<li>
 <li> The equation \"&Delta;p = 0.5*&zeta;*&rho;*v*|v|\" is either with
      respect to port_a or to port_b, depending on the definition
      of the particular loss factor &zeta; (in some references loss
      factors are defined with respect to port_a, in other references
      with respect to port_b).</li>
- 
-<li> Re = |v|*D_Re*&rho;/&eta; = |m_flow|*D_Re/(A_Re*&eta;) 
+
+<li> Re = |v|*D_Re*&rho;/&eta; = |m_flow|*D_Re/(A_Re*&eta;)
      is the Reynolds number at the smallest cross
      section area. This is often at port_a or at port_b, but can
      also be between the two ports. In the record, the diameter
      D_Re of this smallest cross section area has to be provided, as
-     well, as Re_turbulent, the absolute value of the 
+     well, as Re_turbulent, the absolute value of the
      Reynolds number at which
      the turbulent flow starts. If Re_turbulent is different for
      the two flow directions, use the smaller value as Re_turbulent.</li>
-<li> D is the diameter of the pipe. If the pipe has not a 
+<li> D is the diameter of the pipe. If the pipe has not a
      circular cross section, D = 4*A/P, where A is the cross section
      area and P is the wetted perimeter.</li>
 <li> A is the cross section area with A = &pi;(D/2)^2.
@@ -92,8 +92,8 @@ The laminar and the transition region is usually of
 not much technical interest because the operating point is
 mostly in the turbulent regime. For simplification and for
 numercial reasons, this whole region is described by two
-polynomials of third order, one polynomial for m_flow &ge; 0 
-and one for m_flow &lt; 0. The polynomials start at 
+polynomials of third order, one polynomial for m_flow &ge; 0
+and one for m_flow &lt; 0. The polynomials start at
 Re = |m_flow|*4/(&pi;*D_Re*&eta;), where D_Re is the
 smallest diameter between port_a and port_b.
 The common derivative
@@ -109,12 +109,12 @@ are identical at Re = 0. The polynomials are constructed, such that
 they smoothly touch the characteristic curves in the turbulent
 regions. The whole characteristic is therefore <b>continuous</b>
 and has a <b>finite</b>, <b>continuous first derivative everywhere</b>.
-In some cases, the constructed polynomials would \"vibrate\". This is 
+In some cases, the constructed polynomials would \"vibrate\". This is
 avoided by reducing the derivative at Re=0 in such a way that
 the polynomials are guaranteed to be monotonically increasing.
 The used sufficient criteria for monotonicity follows from:
 </p>
- 
+
 <dl>
 <dt> Fritsch F.N. and Carlson R.E. (1980):</dt>
 <dd> <b>Monotone piecewise cubic interpolation</b>.

OpenHydraulics/Basic/BaseClasses/massFlowRate_dp.mo

@@ -14,7 +14,7 @@ algorithm
    dp = 0.5*zeta*d*v*|v|
       = 0.5*zeta*d*1/(d*A)^2 * m_flow * |m_flow|
       = 0.5*zeta/A^2 *1/d * m_flow * |m_flow|
-      = k/d * m_flow * |m_flow| 
+      = k/d * m_flow * |m_flow|
    k  = 0.5*zeta/A^2
       = 0.5*zeta/(pi*(D/2)^2)^2
       = 8*zeta/(pi*D^2)^2
@@ -28,7 +28,7 @@ m_flow := OpenHydraulics.Utilities.regRoot2(
   annotation (smoothOrder=1, Documentation(info="<html>
 <p>
 Compute mass flow rate from constant loss factor and pressure drop (m_flow = f(dp)).
-For small pressure drops (dp &lt; dp_small), the characteristic is approximated by 
+For small pressure drops (dp &lt; dp_small), the characteristic is approximated by
 a polynomial in order to have a finite derivative at zero mass flow rate.
 </p>
 </html>"));

OpenHydraulics/Basic/BaseClasses/massFlowRate_dp_and_Re.mo

@@ -19,31 +19,31 @@ protected
 algorithm
 /*
 Turbulent region:
-   Re = m_flow*(4/pi)/(D_Re*eta)  
+   Re = m_flow*(4/pi)/(D_Re*eta)
    dp = 0.5*zeta*d*v*|v|
       = 0.5*zeta*d*1/(d*A)^2 * m_flow * |m_flow|
       = 0.5*zeta/A^2 *1/d * m_flow * |m_flow|
-      = k/d * m_flow * |m_flow| 
+      = k/d * m_flow * |m_flow|
    k  = 0.5*zeta/A^2
       = 0.5*zeta/(pi*(D/2)^2)^2
       = 8*zeta/(pi*D^2)^2
    m_flow_turbulent = (pi/4)*D_Re*eta*Re_turbulent
    dp_turbulent     =  k/d *(D_Re*eta*pi/4)^2 * Re_turbulent^2
- 
+
    The start of the turbulent region is computed with mean values
    of dynamic viscosity eta and density rho. Otherwise, one has
    to introduce different "delta" values for both flow directions.
-   In order to simplify the approach, only one delta is used.  
- 
+   In order to simplify the approach, only one delta is used.
+
 Laminar region:
    dp = 0.5*zeta/(A^2*d) * m_flow * |m_flow|
       = 0.5 * c0/(|m_flow|*(4/pi)/(D_Re*eta)) / ((pi*(D_Re/2)^2)^2*d) * m_flow*|m_flow|
       = 0.5 * c0*(pi/4)*(D_Re*eta) * 16/(pi^2*D_Re^4*d) * m_flow*|m_flow|
       = 2*c0/(pi*D_Re^3) * eta/d * m_flow
       = k0 * eta/d * m_flow
    k0 = 2*c0/(pi*D_Re^3)
- 
-   In order that the derivative of dp=f(m_flow) is continuous 
+
+   In order that the derivative of dp=f(m_flow) is continuous
    at m_flow=0, the mean values of eta and d are used in the
    laminar region: eta/d = (eta_a + eta_b)/(d_a + d_b)
    If data.zetaLaminarKnown = false then eta_a and eta_b are potentially zero
@@ -70,11 +70,11 @@ is treated as a turbulent flow with constant loss factor zeta.
 If the Reynolds-number Re < data.Re_turbulent, the flow
 is laminar and/or in a transition region between laminar and
 turbulent. This region is approximated by two
-polynomials of third order, one polynomial for m_flow ≥ 0 
-and one for m_flow < 0. 
+polynomials of third order, one polynomial for m_flow ≥ 0
+and one for m_flow < 0.
 The common derivative
 of the two polynomials at Re = 0 is
-computed from the equation \"data.c0/Re\". 
+computed from the equation \"data.c0/Re\".
 </p>
 <p>
 If no data for c0 is available, the derivative at Re = 0 is computed in such
@@ -83,12 +83,12 @@ are identical at Re = 0. The polynomials are constructed, such that
 they smoothly touch the characteristic curves in the turbulent
 regions. The whole characteristic is therefore <b>continuous</b>
 and has a <b>finite</b>, <b>continuous first derivative everywhere</b>.
-In some cases, the constructed polynomials would \"vibrate\". This is 
+In some cases, the constructed polynomials would \"vibrate\". This is
 avoided by reducing the derivative at Re=0 in such a way that
 the polynomials are guaranteed to be monotonically increasing.
 The used sufficient criteria for monotonicity follows from:
 </p>
- 
+
 <dl>
 <dt> Fritsch F.N. and Carlson R.E. (1980):</dt>
 <dd> <b>Monotone piecewise cubic interpolation</b>.

OpenHydraulics/Basic/BaseClasses/pressureLoss_m_flow.mo

@@ -15,7 +15,7 @@ algorithm
    dp = 0.5*zeta*d*v*|v|
       = 0.5*zeta*d*1/(d*A)^2 * m_flow * |m_flow|
       = 0.5*zeta/A^2 *1/d * m_flow * |m_flow|
-      = k/d * m_flow * |m_flow| 
+      = k/d * m_flow * |m_flow|
    k  = 0.5*zeta/A^2
       = 0.5*zeta/(pi*(D/2)^2)^2
       = 8*zeta/(pi*D^2)^2
@@ -28,7 +28,7 @@ dp := OpenHydraulics.Utilities.regSquare2(
   annotation (smoothOrder=1, Documentation(info="<html>
 <p>
 Compute pressure drop from constant loss factor and mass flow rate (dp = f(m_flow)).
-For small mass flow rates(|m_flow| &lt; m_flow_small), the characteristic is approximated by 
+For small mass flow rates(|m_flow| &lt; m_flow_small), the characteristic is approximated by
 a polynomial in order to have a finite derivative at zero mass flow rate.
 </p>
 </html>"));

OpenHydraulics/Basic/BaseClasses/pressureLoss_m_flow_and_Re.mo

@@ -19,31 +19,31 @@ protected
 algorithm
 /*
 Turbulent region:
-   Re = m_flow*(4/pi)/(D_Re*eta)  
+   Re = m_flow*(4/pi)/(D_Re*eta)
    dp = 0.5*zeta*d*v*|v|
       = 0.5*zeta*d*1/(d*A)^2 * m_flow * |m_flow|
       = 0.5*zeta/A^2 *1/d * m_flow * |m_flow|
-      = k/d * m_flow * |m_flow| 
+      = k/d * m_flow * |m_flow|
    k  = 0.5*zeta/A^2
       = 0.5*zeta/(pi*(D/2)^2)^2
       = 8*zeta/(pi*D^2)^2
    m_flow_turbulent = (pi/4)*D_Re*eta*Re_turbulent
    dp_turbulent     =  k/d *(D_Re*eta*pi/4)^2 * Re_turbulent^2
- 
+
    The start of the turbulent region is computed with mean values
    of dynamic viscosity eta and density rho. Otherwise, one has
    to introduce different "delta" values for both flow directions.
-   In order to simplify the approach, only one delta is used.  
- 
+   In order to simplify the approach, only one delta is used.
+
 Laminar region:
    dp = 0.5*zeta/(A^2*d) * m_flow * |m_flow|
       = 0.5 * c0/(|m_flow|*(4/pi)/(D_Re*eta)) / ((pi*(D_Re/2)^2)^2*d) * m_flow*|m_flow|
       = 0.5 * c0*(pi/4)*(D_Re*eta) * 16/(pi^2*D_Re^4*d) * m_flow*|m_flow|
       = 2*c0/(pi*D_Re^3) * eta/d * m_flow
       = k0 * eta/d * m_flow
    k0 = 2*c0/(pi*D_Re^3)
- 
-   In order that the derivative of dp=f(m_flow) is continuous 
+
+   In order that the derivative of dp=f(m_flow) is continuous
    at m_flow=0, the mean values of eta and d are used in the
    laminar region: eta/d = (eta_a + eta_b)/(d_a + d_b)
    If data.zetaLaminarKnown = false then eta_a and eta_b are potentially zero
@@ -67,11 +67,11 @@ is treated as a turbulent flow with constant loss factor zeta.
 If the Reynolds-number Re < data.Re_turbulent, the flow
 is laminar and/or in a transition region between laminar and
 turbulent. This region is approximated by two
-polynomials of third order, one polynomial for m_flow ≥ 0 
-and one for m_flow < 0. 
+polynomials of third order, one polynomial for m_flow ≥ 0
+and one for m_flow < 0.
 The common derivative
 of the two polynomials at Re = 0 is
-computed from the equation \"data.c0/Re\". 
+computed from the equation \"data.c0/Re\".
 </p>
 <p>
 If no data for c0 is available, the derivative at Re = 0 is computed in such
@@ -80,12 +80,12 @@ are identical at Re = 0. The polynomials are constructed, such that
 they smoothly touch the characteristic curves in the turbulent
 regions. The whole characteristic is therefore <b>continuous</b>
 and has a <b>finite</b>, <b>continuous first derivative everywhere</b>.
-In some cases, the constructed polynomials would \"vibrate\". This is 
+In some cases, the constructed polynomials would \"vibrate\". This is
 avoided by reducing the derivative at Re=0 in such a way that
 the polynomials are guaranteed to be monotonically increasing.
 The used sufficient criteria for monotonicity follows from:
 </p>
- 
+
 <dl>
 <dt> Fritsch F.N. and Carlson R.E. (1980):</dt>
 <dd> <b>Monotone piecewise cubic interpolation</b>.

OpenHydraulics/Basic/WallFriction.mo

@@ -55,12 +55,12 @@ The details are described in the
 The functional relationship of the friction loss factor λ is
 displayed in the next figure. Function massFlowRate_dp() defines the \"red curve\"
 (\"Swamee and Jain\"), where as function pressureLoss_m_flow() defines the
-\"blue curve\" (\"Colebrook-White\"). The two functions are inverses from 
+\"blue curve\" (\"Colebrook-White\"). The two functions are inverses from
 each other and give slightly different results in the transition region
 between Re = 1500 .. 4000, in order to get explicit equations without
 solving a non-linear equation.
 </p>
- 
+
 <img src=\"../Images/Components/PipeFriction1.png\">
 </html>"));
 end WallFriction;

OpenHydraulics/Basic/package.mo

@@ -4,22 +4,21 @@ package Basic "Models of basic physical phenomena relevant to the hydraulics dom
 
 
   annotation (Documentation(info="<html>
-<h4><font color=\"#008000\" size=5>Overview</font></h4>  
-<p>The OpenHydraulics/Basic package includes models of basic physical phenomena relevant to the hydraulics domain.  
+<h4><font color=\"#008000\" size=5>Overview</font></h4>
+<p>The OpenHydraulics/Basic package includes models of basic physical phenomena relevant to the hydraulics domain.
 These basic models are used in the components package to model actual hydraulic components.</p>
 <h4><font color=\"#008000\" size=5>Licensing</font></h4>
 <p>
 The OpenHydraulics/Basic package is licensed by Georgia Institute of Technology under the
-<a href=\"http://www.modelica.org/licenses/ModelicaLicense2\"><b>Modelica License 2</b></a>.</p> 
+<a href=\"http://www.modelica.org/licenses/ModelicaLicense2\"><b>Modelica License 2</b></a>.</p>
 <p><b>Copyright &copy; 2008-2013, Georgia Insitute of Technology</b>
 </p>
 <p>
-This Modelica package is free software and the use is completely at your own risk; 
-it can be redistributed and/or modified under the terms of the Modelica License 2. 
-For license conditions (including the disclaimer of warranty) see 
-<a href=\"modelica://Hydraulics.UsersGuide.ModelicaLicense2\">Hydraulics.UsersGuide.ModelicaLicense2</a> or visit 
+This Modelica package is free software and the use is completely at your own risk;
+it can be redistributed and/or modified under the terms of the Modelica License 2.
+For license conditions (including the disclaimer of warranty) see
+<a href=\"modelica://Hydraulics.UsersGuide.ModelicaLicense2\">Hydraulics.UsersGuide.ModelicaLicense2</a> or visit
 <a href=\"http://www.modelica.org/licenses/ModelicaLicense2\">http://www.modelica.org/licenses/ModelicaLicense2</a>.
 </p>
-</html>
-"));
+</html>"));
 end Basic;

OpenHydraulics/Circuits/package.mo

@@ -6,21 +6,20 @@ package Circuits "A collection of simple and complex hydraulic circuits"
 
 
     annotation (Documentation(info="<html>
-<h4><font color=\"#008000\" size=5>Overview</font></h4>  
+<h4><font color=\"#008000\" size=5>Overview</font></h4>
 <p>The OpenHydraulics/Circuits package includes a collection of simple and complex hydraulic circuits.</p>
 <h4><font color=\"#008000\" size=5>Licensing</font></h4>
 <p>
 The OpenHydraulics/Circuits package is licensed by Georgia Institute of Technology under the
-<a href=\"http://www.modelica.org/licenses/ModelicaLicense2\"><b>Modelica License 2</b></a>.</p> 
+<a href=\"http://www.modelica.org/licenses/ModelicaLicense2\"><b>Modelica License 2</b></a>.</p>
 <p><b>Copyright &copy; 2008-2013, Georgia Insitute of Technology</b>
 </p>
 <p>
-This Modelica package is free software and the use is completely at your own risk; 
-it can be redistributed and/or modified under the terms of the Modelica License 2. 
-For license conditions (including the disclaimer of warranty) see 
-<a href=\"modelica://Hydraulics.UsersGuide.ModelicaLicense2\">Hydraulics.UsersGuide.ModelicaLicense2</a> or visit 
+This Modelica package is free software and the use is completely at your own risk;
+it can be redistributed and/or modified under the terms of the Modelica License 2.
+For license conditions (including the disclaimer of warranty) see
+<a href=\"modelica://Hydraulics.UsersGuide.ModelicaLicense2\">Hydraulics.UsersGuide.ModelicaLicense2</a> or visit
 <a href=\"http://www.modelica.org/licenses/ModelicaLicense2\">http://www.modelica.org/licenses/ModelicaLicense2</a>.
 </p>
-</html>
-"));
+</html>"));
 end Circuits;

OpenHydraulics/Components/Cylinders/BaseClasses/package.mo

@@ -1,4 +1,4 @@
 within OpenHydraulics.Components.Cylinders;
-package BaseClasses 
+package BaseClasses
   extends Modelica.Icons.BasesPackage;
 end BaseClasses;

OpenHydraulics/Components/Cylinders/package.mo

@@ -1,5 +1,5 @@
 within OpenHydraulics.Components;
-package Cylinders 
+package Cylinders
   extends OpenHydraulics.Interfaces.VariantLibrary;
 
 end Cylinders;

OpenHydraulics/Components/Lines/Line.mo

@@ -112,7 +112,7 @@ equation
             fillPattern=FillPattern.Solid,
             textString="A")}),             Documentation(info="<html>
 <p>
-Simple pipe model consisting of one volume, 
+Simple pipe model consisting of one volume,
 wall friction (with different friction correlations)
 and gravity effect. This model is mostly used to demonstrate how
 to build up more detailed models from the basic components.

OpenHydraulics/Components/Lines/package.mo

@@ -1,5 +1,5 @@
 within OpenHydraulics.Components;
-package Lines 
+package Lines
   extends OpenHydraulics.Interfaces.VariantLibrary;
 
 end Lines;

OpenHydraulics/Components/MotorsPumps/BaseClasses/MechanicalPumpLosses.mo

@@ -61,8 +61,7 @@ Part B, Vol. 198, No. 10, 1984, pp 165-174.
 The model implementation is derived from the bearing friction
 model in the standard Modelica library.
 </p>
-</HTML>
-"), Window(
+</html>"), Window(
       x=0.25,
       y=0.01,
       width=0.53,

OpenHydraulics/Components/MotorsPumps/BaseClasses/package.mo

@@ -1,4 +1,4 @@
 within OpenHydraulics.Components.MotorsPumps;
-package BaseClasses 
+package BaseClasses
   extends Modelica.Icons.BasesPackage;
 end BaseClasses;

OpenHydraulics/Components/MotorsPumps/package.mo

@@ -1,5 +1,5 @@
 within OpenHydraulics.Components;
-package MotorsPumps 
+package MotorsPumps
   extends OpenHydraulics.Interfaces.VariantLibrary;
 
 end MotorsPumps;

OpenHydraulics/Components/Sensors/package.mo

@@ -1,5 +1,5 @@
 within OpenHydraulics.Components;
-package Sensors 
+package Sensors
   extends OpenHydraulics.Interfaces.VariantLibrary;
 
 end Sensors;

OpenHydraulics/Components/Valves/DirectionalValves/BaseClasses/package.mo

@@ -1,5 +1,5 @@
 within OpenHydraulics.Components.Valves.DirectionalValves;
-package BaseClasses 
+package BaseClasses
   extends Modelica.Icons.BasesPackage;